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Depends on the fuel. Type of engine is not important.
For gasoline, a 16:1 ratio would be ideal, for alcohol (Ethanol) 8:1 is considered ideal.
A good estimate for any fuel is to split the difference between Lower Explosive Limit (won't burn; too lean) and Upper Explosive Limit (won't burn, too rich). For example, Propane has a LEL of 24,000 ppm, and HEL of 96,000 ppm, so split the difference and 60,000 ppm should burn pretty well.
60,000 ppm should be about 6% or 17:1.
What else can I help you with?
What is bypass ratio of turbine?
The bypass ratio of a turbine, particularly in the context of turbofan engines, is the ratio of the mass of air that bypasses the engine core to the mass of air that passes through the engine core. A higher bypass ratio indicates that more air is bypassed, typically resulting in greater fuel efficiency and lower noise levels. Turbofans with high bypass ratios are commonly used in commercial aviation, while those with lower ratios are found in military and supersonic aircraft.
What is bleeding of turbine?
Bleed air in gas turbine engines is compressed air taken from within the engine, after the compressor stage(s) and before the fuel is injected in the burner
What is the Airflow or a turbine engine?
Airflow in a turbine engine refers to the movement of air through the engine's various components, including the intake, compressor, combustion chamber, and turbine. This airflow is crucial for the engine's operation, as it facilitates the combustion of fuel and the generation of thrust. The compressor increases the pressure of incoming air, while the turbine extracts energy from the high-temperature exhaust gases, driving the compressor and producing thrust. Efficient airflow management is essential for maximizing performance and fuel efficiency in turbine engines.
The main purpose of the turbine in the turbojet engine is to?
The major function of the turbine in the turbojet is that it supplies the power to turn the compressor. An automatic fuel control unit on a turbojet engine is influenced by the burner pressure.
How does a jet engine create thrust?
There are a few different jet engines, but it basically needs bleed air and fuel. Air enters the engine where it is compressed and mixed with fuel. Next, the air/fuel is heated in a combustion chamber, then it is unleashed through the turbine as thrust.
The air fuel ratio of the petrol engine is controlled by?
The air fuel ratio of the petrol engine is controlled by Carburetor
What is the fuel-air ratio in a jet engine?
The ratio is about 15:1 fuel to air.
What is the air fuel ratio in petrol engine?
Ideally it is 14.7 air to 1 fuel in an internal combustion engine.
What is bypass ratio of turbine?
The bypass ratio of a turbine, particularly in the context of turbofan engines, is the ratio of the mass of air that bypasses the engine core to the mass of air that passes through the engine core. A higher bypass ratio indicates that more air is bypassed, typically resulting in greater fuel efficiency and lower noise levels. Turbofans with high bypass ratios are commonly used in commercial aviation, while those with lower ratios are found in military and supersonic aircraft.
What is bleeding of turbine?
Bleed air in gas turbine engines is compressed air taken from within the engine, after the compressor stage(s) and before the fuel is injected in the burner
What is stiochiometric air fuel ratio?
It is when the "correct" air to fuel ratio is used to completely burn the fuel in question in an internal combustion engine. If exactly the correct amount of air is used this is called the stoichiometric mix.
What is the Airflow or a turbine engine?
Airflow in a turbine engine refers to the movement of air through the engine's various components, including the intake, compressor, combustion chamber, and turbine. This airflow is crucial for the engine's operation, as it facilitates the combustion of fuel and the generation of thrust. The compressor increases the pressure of incoming air, while the turbine extracts energy from the high-temperature exhaust gases, driving the compressor and producing thrust. Efficient airflow management is essential for maximizing performance and fuel efficiency in turbine engines.
The main purpose of the turbine in the turbojet engine is to?
The major function of the turbine in the turbojet is that it supplies the power to turn the compressor. An automatic fuel control unit on a turbojet engine is influenced by the burner pressure.
A smoothly operating engine depends on?
A 14.7 to 1 air/fuel ratio.
How does a jet engine create thrust?
There are a few different jet engines, but it basically needs bleed air and fuel. Air enters the engine where it is compressed and mixed with fuel. Next, the air/fuel is heated in a combustion chamber, then it is unleashed through the turbine as thrust.
The turbulence in diesel engine ensures to?
Ensures that all the fuel mixes with the air creating a proper air to fuel ratio to produce combustion.
What is a servo regulator in aircraft?
Regulates the amount of fuel to the engine to maintain the fuel/air ratio at the proper mixture
